Multi-rotor manned aircraft

Abstract

The invention discloses a multi-rotor manned vehicle, comprising man-carried cabin, lifting rotor, equipment bin and steering rudder; the upper part of the said man-carried cabin is provided with a window, the bottom edge is provided with a landing gear or taxiing wheels, the outer wall is provided with a cabin door, the outer wall of both sides or the top is provided with a side-push rotor separately, and the back end of the said side-push rotor is provided with a first power device to drive the said side-push rotor; the said lifting rotors are provided of a quantity of at least two, which are arranged side-by-side in parallel around or on both sides of the said man-carried cabin, and the lower end of each said lifting rotor is respectively provided with a second power device to drive the said lifting rotor; the said equipment bin is arranged at the bottom of the said man-carried cabin, in which a power source is provided for the operation of the said first power device and the second power device; the said steering rudder is arranged at the rear or top of the said man-carried cabin. The flight, take-off and landing of the invention is similar to the unmanned aerial vehicle, having the advantages of small and flexible, low altitude and low speed, vertical lifting, economic and practical.

1 . A multi-rotor manned vehicle, characterized by: including man-carried cabin ( 1 ), lifting rotor ( 5 ), equipment cabin ( 8 ) and steering rudder ( 10 );
 The upper part of the said man-carried cabin ( 1 ) is provided with a window ( 7 ), the bottom edge is provided with a landing gear or taxiing wheels ( 9 ), the outer wall is provided with a cabin door ( 4 ), the outer wall of both sides or the top is provided with a side-push rotor ( 2 ) separately, and the back end of the said side-push rotor ( 2 ) is provided with a first power device ( 3 ) to drive the said side-push rotor ( 2 );   The said lifting rotors ( 5 ) are provided of a quantity of at least two, which are arranged side-by-side in parallel around or on both sides of the said man-carried cabin ( 1 ), and the lower end of each said lifting rotor ( 5 ) is respectively provided with a second power device ( 6 ) to drive the said lifting rotor ( 5 );   The said equipment bin ( 8 ) is arranged at the bottom of the said man-carried cabin ( 1 ), in which a power source is provided for the operation of the said first power device ( 3 ) and the second power device ( 6 );   The said steering rudder ( 10 ) is arranged at the rear or top of the said man-carried cabin ( 1 ).   
     
     
         2 . According to the multi-rotor manned vehicle described in  claim 1 , characterized by: the said man-carried cabin ( 1 ) is of a capsule structure with a circular cross section to accommodate a single person, or a strip section to accommodate three people, or a rectangle section to accommodate more than three people, or a boat-shape section to accommodate more than three people. 
     
     
         3 . According to the multi-rotor manned vehicle described in  claim 1 , characterized by: a parachute ( 11 ) is arranged at the top of the said man-carried cabin ( 1 ). 
     
     
         4 . According to the multi-rotor manned vehicle described in  claim 1 , characterized by: a first guide tube cover ( 12 ) is arranged vertically outside the said lifting rotor ( 5 ). 
     
     
         5 . According to the multi-rotor manned vehicle described in  claim 1  or  4 , characterized by: each said lifting rotor ( 5 ) is arranged side by side in parallel around or on both sides of the said man-carried cabin ( 1 ) and is connected with the outer wall corresponding to the said man-carried cabin ( 1 ) by a connecting arm. 
     
     
         6 . According to the multi-rotor manned vehicle described in  claim 1 , characterized by: a second guide tube cover ( 13 ) is arranged horizontally outside the said side-push rotor ( 2 ). 
     
     
         7 . According to the multi-rotor manned vehicle described in  claim 1 , characterized by: both the said first power device ( 3 ) and second power device ( 6 ) are driven by engines or electric motors. 
     
     
         8 . According to the multi-rotor manned vehicle described in  claim 7 , characterized by: when both the said first power device ( 3 ) and second power device ( 6 ) are driven by engines, the said power source is fuel; when both the said first power device ( 3 ) and second power device ( 6 ) are driven by electric motors, the said power source is storage battery. 
     
     
         9 . According to the multi-rotor manned vehicle described in  claim 1 , characterized by: the said landing gear or taxiing wheels ( 9 ) is provided with a function of shock absorption.